| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 721624 | IFAC Proceedings Volumes | 2007 | 6 Pages |
Abstract
The paper describes a model based approach to provide an integrated structural coupling filter for a military aircraft. It utilises a steady-state version of the well-known Kalman filter, designed using a model containing rigid and flexible modes relevant to longitudinal dynamics, and provides an important alternative to the existing approach using a number of notch filters in the sensor and actuator paths.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
